捷联惯导半实物仿真测试系统研究  

Hardware-in-the-Loop Simulation for Test System of Missile Strapdown Inertial Navigation System

作　　者：白云[1] 黄孝文[1,2] 赵俊峰[1] 

机构地区：[1]空军工程大学导弹学院 [2]中国人民解放军94907部队

出　　处：《航天控制》2010年第3期56-59,64,共5页Aerospace Control

摘　　要：根据当前某型防空导弹捷联惯导系统测试及仿真现状,提出了一种建立在自动测试基础之上的导弹稳定回路半物理仿真系统方案。在该方案中,采用工控机和分布式实时网络,并充分利用计算机仿真技术和虚拟仪器技术,有效地结合二者的功能,使这个系统平台既能够实现对捷联惯导系统综合测试,又能通过仿真来验证导弹控制律的优劣,成为一个高精度、多用途、具有实时自诊断功能的测试和仿真系统平台。由于系统基于模块化设计,因此具有良好的通用性和很强的可扩展性,能够通过更换适配器来完成不同型号导弹的测试和仿真任务。According to the current situation of strapdown inertial navigation equipment testing for certain type anti-aircraft missile,a scheme of hardware-in-the-loop simulation system for missile stable loop based on automatic test system is presented.By making use of virtual system and computer simulation technologies,a test and simulation system with high precision,multi-purposes and self-diagnosis capabilities is built up.The system not only can accomplish the integrative test of strapdown inertial navigation equipments,but also can classify the performance of missile stable loop.The system proposed in this paper can carry out the missions of testing different missiles and also can be easily extended by changing the different adapters.

关 键 词：导弹 捷联惯导 自动测试 半实物仿真 

分 类 号：V448.153[航空宇航科学与技术—飞行器设计]